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BR9911653A - Sistema de controle de trajetória de balão - Google Patents

Sistema de controle de trajetória de balão

Info

Publication number
BR9911653A
BR9911653A BR9911653-7A BR9911653A BR9911653A BR 9911653 A BR9911653 A BR 9911653A BR 9911653 A BR9911653 A BR 9911653A BR 9911653 A BR9911653 A BR 9911653A
Authority
BR
Brazil
Prior art keywords
balloon
force
wing
control
tether
Prior art date
Application number
BR9911653-7A
Other languages
English (en)
Inventor
Kim Maynard Aaron
Original Assignee
Global Aerospace Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=22312099&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=BR9911653(A) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Global Aerospace Corp filed Critical Global Aerospace Corp
Publication of BR9911653A publication Critical patent/BR9911653A/pt

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Wind Motors (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Steering Control In Accordance With Driving Conditions (AREA)
  • Percussion Or Vibration Massage (AREA)

Abstract

Patente de Invenção: <B>"SISTEMA DE CONTROLE DE TRAJETóRIA DE BALãO"<D>. Um dispositivo para proporcionar o controle da trajetória de um veículo mais leve do que o ar, tal como um balão, é produzido. Um dispositivo de elevação, tal como uma asa na extremidade, é suspenso em uma corda bem abaixo do balão para tirar vantagem da variação natural nos ventos em diferentes altitudes. A asa pode gerar uma força de elevação horizontal que pode ser direcionada sobre uma ampla faixa de ângulos. Essa força é transmitida para o balão pela corda. Devido a essa força, a trajetória do balão é alterada dependendo dos tamanhos relativos do balão e da asa. Uma quantidade relativamente pequena de energia é necessária para controlar o sistema, possivelmente com um leme. Já que a energia do vento produz a maior parte da força, a energia do vento faz a maior parte do trabalho. O balão é capaz de evitar perigos, de alcançar alvos desejados, de selecionar zonas de aterrissagem convenientes e de proporcionar outras vantagens operacionais. Como resultado, poucos vóos devem ser terminados antecipadamente devido a uma incapacidade de controlar a trajetória e é mais fácil obter permissão para lançamento desde que uma trajetória de vóo planejada pode ser atingida dentro de uma maior faixa de condições.
BR9911653-7A 1998-06-29 1999-06-25 Sistema de controle de trajetória de balão BR9911653A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/106,563 US6402090B1 (en) 1998-06-29 1998-06-29 Balloon trajectory control system
PCT/US1999/014430 WO2000000387A2 (en) 1998-06-29 1999-06-25 Balloon trajectory control system

Publications (1)

Publication Number Publication Date
BR9911653A true BR9911653A (pt) 2001-10-09

Family

ID=22312099

Family Applications (1)

Application Number Title Priority Date Filing Date
BR9911653-7A BR9911653A (pt) 1998-06-29 1999-06-25 Sistema de controle de trajetória de balão

Country Status (13)

Country Link
US (1) US6402090B1 (pt)
EP (1) EP1144247B1 (pt)
JP (1) JP4505139B2 (pt)
CN (1) CN1168630C (pt)
AT (1) ATE267117T1 (pt)
AU (1) AU764203B2 (pt)
BR (1) BR9911653A (pt)
CA (1) CA2335954C (pt)
DE (1) DE69917487D1 (pt)
HK (1) HK1040224B (pt)
NZ (1) NZ509377A (pt)
RU (1) RU2238217C2 (pt)
WO (1) WO2000000387A2 (pt)

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US8849571B1 (en) 2012-12-26 2014-09-30 Google Inc. Methods and systems for determining fleet trajectories with phase-skipping to satisfy a sequence of coverage requirements
US9747568B1 (en) 2012-12-26 2017-08-29 X Development Llc Methods and systems for determining when to decommission vehicles from a fleet of autonomous vehicles
US9195938B1 (en) 2012-12-27 2015-11-24 Google Inc. Methods and systems for determining when to launch vehicles into a fleet of autonomous vehicles
US8948927B1 (en) 2012-12-27 2015-02-03 Google Inc. Methods and systems for determining a distribution of balloons based on population densities
US8862403B1 (en) 2012-12-28 2014-10-14 Google Inc. Methods and systems for determining altitudes for a vehicle to travel
US9014957B2 (en) 2012-12-29 2015-04-21 Google Inc. Methods and systems for determining fleet trajectories to satisfy a sequence of coverage requirements
US9635706B1 (en) 2013-01-02 2017-04-25 X Development Llc Method for determining fleet control policies to satisfy a sequence of coverage requirements
WO2014109917A1 (en) * 2013-01-10 2014-07-17 Leonid Goldstein Airborne wind energy system
US8781727B1 (en) 2013-01-15 2014-07-15 Google Inc. Methods and systems for performing flocking while executing a long-range fleet plan
US8874356B1 (en) 2013-01-24 2014-10-28 Google Inc. Methods and systems for decomposing fleet planning optimizations via spatial partitions
US8880326B1 (en) 2013-02-20 2014-11-04 Google Inc. Methods and systems for determining a cyclical fleet plan satisfying a recurring set of coverage requirements
CN103661915B (zh) * 2013-11-18 2015-12-30 中国空间技术研究院 一种自然热和帆驱动的轨迹可控浮空器系统
US9201426B1 (en) * 2014-02-19 2015-12-01 Google Inc. Reverse iteration of planning data for system control
US9789960B2 (en) 2015-01-14 2017-10-17 Raymond Hoheisel Payload orientation control and stabilization
WO2016137525A1 (en) * 2015-02-27 2016-09-01 Ocean Lab, Llc A reconfigurable drift measurement tool
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US9665103B1 (en) 2015-12-09 2017-05-30 X Development Llc Efficient aerostat navigation by moving between atmospheric layers
US10118696B1 (en) 2016-03-31 2018-11-06 Steven M. Hoffberg Steerable rotating projectile
US10759535B2 (en) 2016-06-14 2020-09-01 Raymond Hoheisel Airborne launch of inflatable devices
CN107867386B (zh) * 2016-09-28 2022-06-03 深圳光启空间技术有限公司 浮空器的降落控制方法
US10809718B2 (en) 2017-07-28 2020-10-20 Loon Llc Systems and methods for controlling aerial vehicles
US10437259B2 (en) * 2017-07-28 2019-10-08 Loon Llc Systems and methods for controlling aerial vehicles
US10437260B2 (en) 2017-07-28 2019-10-08 Loon Llc Systems and methods for controlling aerial vehicles
US10558219B2 (en) 2017-09-21 2020-02-11 Loon Llc Systems and methods for controlling an aerial vehicle using lateral propulsion and vertical movement
US10780969B2 (en) 2017-12-21 2020-09-22 Loon Llc Propulsion system for a buoyant aerial vehicle
US11712637B1 (en) 2018-03-23 2023-08-01 Steven M. Hoffberg Steerable disk or ball
RU2712468C1 (ru) * 2019-03-22 2020-01-29 ФЕДЕРАЛЬНОЕ ГОСУДАРСТВЕННОЕ КАЗЕННОЕ ВОЕННОЕ ОБРАЗОВАТЕЛЬНОЕ УЧРЕЖДЕНИЕ ВЫСШЕГО ОБРАЗОВАНИЯ "Военная академия Ракетных войск стратегического назначения имени Петра Великого" МИНИСТЕРСТВА ОБОРОНЫ РОССИЙСКОЙ ФЕДЕРАЦИИ Система обнаружения воздушных и наземных целей
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Also Published As

Publication number Publication date
HK1040224A1 (en) 2002-05-31
JP4505139B2 (ja) 2010-07-21
ATE267117T1 (de) 2004-06-15
CN1322176A (zh) 2001-11-14
JP2002519236A (ja) 2002-07-02
WO2000000387A3 (en) 2001-12-13
EP1144247A3 (en) 2002-03-06
WO2000000387A2 (en) 2000-01-06
AU4832999A (en) 2000-01-17
RU2238217C2 (ru) 2004-10-20
CA2335954A1 (en) 2000-01-06
US6402090B1 (en) 2002-06-11
DE69917487D1 (de) 2004-06-24
CA2335954C (en) 2007-04-24
EP1144247B1 (en) 2004-05-19
NZ509377A (en) 2003-08-29
CN1168630C (zh) 2004-09-29
AU764203B2 (en) 2003-08-14
HK1040224B (zh) 2005-05-20
EP1144247A2 (en) 2001-10-17

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Legal Events

Date Code Title Description
B06A Patent application procedure suspended [chapter 6.1 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 25/06/1999, OBSERVADAS AS CONDICOES LEGAIS.

B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time

Free format text: REFERENTE A 20A ANUIDADE.

B24J Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12)

Free format text: EM VIRTUDE DA EXTINCAO PUBLICADA NA RPI 2520 DE 25-04-2019 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDA A EXTINCAO DA PATENTE E SEUS CERTIFICADOS, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.